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Newtonian Mechanics Review | Physics

sources:

  • text: “Halliday, D., Resnick, R., & Walker, J. (2013). Fundamentals of Physics (10th ed.). Wiley.”
  • text: “Serway, R. A., & Jewett, J. W. (2018). Physics for Scientists and Engineers (10th ed.). Cengage Learning.”

Kinematics is the study of motion without asking why it happens. Position, velocity, and acceleration are three successive derivatives of time, but they tell three different stories about the same motion. Position answers “where is the object?” — it is the raw record of location at each instant. Velocity answers “how is the position changing?” — it is the rate and direction of that change. Acceleration answers “how is the velocity changing?” — it captures the tendency of the motion itself to evolve.

The physical metaphor is a car journey. The odometer reading at each moment is the position. The speedometer reading is the velocity — how fast the position is changing. The accelerometer reading is the acceleration — whether you are pressing the brake or the accelerator, and by how much. A car moving at constant velocity has zero acceleration: the story of its motion is complete and unchanging. A car in free fall has constant acceleration g: its velocity story changes at a steady rate, and its position story is a parabola. The key insight is that acceleration is the most fundamental of the three because it is directly caused by forces (Newton’s second law), while velocity and position are consequences that follow by integration.

Newton’s second law, F=ma, is the universe’s accounting rule for motion. It states that the net force on an object equals its mass times its acceleration — or more precisely, the net force equals the rate of change of momentum. The metaphor is a financial ledger: force is the “income” or “expense” applied to an object, mass is the “inertia” (resistance to change in its state of motion), and acceleration is the resulting “change in balance.” Just as a large bank account responds slowly to small deposits, a massive object responds slowly to small forces.

The first law is the special case of zero net force: the ledger is balanced, and the object’s state of motion does not change. The third law is the double-entry bookkeeping principle: every force has an equal and opposite counterpart, so the total “debt” in the universe is always zero. The conservation laws — of momentum, energy, and angular momentum — are the consequences of this accounting system applied to isolated systems. They are the reason we can predict the outcome of a collision without knowing every microscopic detail: the ledger must balance, regardless of the complexity of the transactions.

  1. First Law (Inertia): A body remains at rest or in uniform motion unless acted upon by a net force.
  2. Second Law: F=ma=p˙\mathbf{F} = m\mathbf{a} = \dot{\mathbf{p}} where p=mv\mathbf{p} = m\mathbf{v}.
  3. Third Law: For every action, there is an equal and opposite reaction.

1.2 Newton’s Second Law in Various Coordinate Systems

Section titled “1.2 Newton’s Second Law in Various Coordinate Systems”

In Cartesian coordinates the component equations are straightforward:

Fx=mx¨,Fy=my¨,Fz=mz¨F_x = m\ddot{x}, \quad F_y = m\ddot{y}, \quad F_z = m\ddot{z}

In planar polar coordinates (r,ϕ)(r, \phi)The acceleration decomposes into radial and transverse components:

a=(r¨rϕ˙2)r^+(rϕ¨+2r˙ϕ˙)ϕ^\mathbf{a} = (\ddot{r} - r\dot{\phi}^2)\,\hat{\mathbf{r}} + (r\ddot{\phi} + 2\dot{r}\dot{\phi})\,\hat{\boldsymbol{\phi}}

So Newton’s second law becomes:

Fr=m(r¨rϕ˙2),Fϕ=m(rϕ¨+2r˙ϕ˙)F_r = m(\ddot{r} - r\dot{\phi}^2), \quad F_\phi = m(r\ddot{\phi} + 2\dot{r}\dot{\phi})

The term mrϕ˙2-mr\dot{\phi}^2 is the centrifugal acceleration and 2mr˙ϕ˙2m\dot{r}\dot{\phi} is the Coriolis acceleration.

In cylindrical coordinates (ρ,ϕ,z)(\rho, \phi, z):

a=(ρ¨ρϕ˙2)ρ^+(ρϕ¨+2ρ˙ϕ˙)ϕ^+z¨z^\mathbf{a} = (\ddot{\rho} - \rho\dot{\phi}^2)\,\hat{\boldsymbol{\rho}} + (\rho\ddot{\phi} + 2\dot{\rho}\dot{\phi})\,\hat{\boldsymbol{\phi}} + \ddot{z}\,\hat{\mathbf{z}}

1.3 Worked Example: Block on an Inclined Plane with Friction

Section titled “1.3 Worked Example: Block on an Inclined Plane with Friction”

Problem. A block of mass mm slides down an inclined plane at angle α\alpha to the horizontal. The coefficient of kinetic friction is μk\mu_k. Find the acceleration.

Solution. Choose axes parallel and perpendicular to the incline. The normal force is N=mgcosαN = mg\cos\alpha. The friction force is f=μkN=μkmgcosαf = \mu_k N = \mu_k mg\cos\alpha directed up the plane. Newton’s second law along the plane:

ma=mgsinαμkmgcosαma = mg\sin\alpha - \mu_k mg\cos\alpha

a=g(sinαμkcosα)a = g(\sin\alpha - \mu_k \cos\alpha)

The block accelerates when tanα>μk\tan\alpha \gt \mu_k and decelerates otherwise. \blacksquare

Problem. A mass mm is attached to a string of length ll and rotates in a horizontal circle of radius rr with the string making angle θ\theta with the vertical. Find the angular velocity ω\omega.

Solution. The forces on the mass are tension T\mathbf{T} along the string and weight mgmg downward. Newton’s second law in the vertical direction:

Tcosθmg=0    T=mgcosθT\cos\theta - mg = 0 \implies T = \frac{mg}{\cos\theta}

In the radial (horizontal) direction:

Tsinθ=mω2r=mω2lsinθT\sin\theta = m\omega^2 r = m\omega^2 l\sin\theta

mgcosθsinθ=mω2lsinθ\frac{mg}{\cos\theta}\sin\theta = m\omega^2 l\sin\theta

ω2=glcosθ\omega^2 = \frac{g}{l\cos\theta}

The period is T=2π/ω=2πlcosθ/gT = 2\pi/\omega = 2\pi\sqrt{l\cos\theta/g}. \blacksquare

Theorem 1.1 (Conservation of Linear Momentum). For a system of NN particles with no external forces, the total linear momentum is conserved.

Proof. Newton’s second law for the ii-th particle:

Fi(ext)+jiFij=miv˙i\mathbf{F}_i^{(\mathrm{ext})} + \sum_{j \neq i} \mathbf{F}_{ij} = m_i \dot{\mathbf{v}}_i

Where Fij\mathbf{F}_{ij} is the force on particle ii due to particle jj. By Newton’s third law, Fij=Fji\mathbf{F}_{ij} = -\mathbf{F}_{ji}. Summing over all particles:

iFi(ext)+ijiFij=ddtimivi\sum_i \mathbf{F}_i^{(\mathrm{ext})} + \sum_i \sum_{j \neq i} \mathbf{F}_{ij} = \frac{d}{dt}\sum_i m_i \mathbf{v}_i

The double sum vanishes by Newton’s third law. Defining P=imivi\mathbf{P} = \sum_i m_i \mathbf{v}_i:

iFi(ext)=P˙\sum_i \mathbf{F}_i^{(\mathrm{ext})} = \dot{\mathbf{P}}

If there are no external forces, P˙=0\dot{\mathbf{P}} = 0 and P\mathbf{P} is constant. \blacksquare

Corollary. The centre of mass moves as if all external forces acted on a single particle of mass M=imiM = \sum_i m_i located at the centre of mass: MR¨=iFi(ext)M\ddot{\mathbf{R}} = \sum_i \mathbf{F}_i^{(\mathrm{ext})}.

Theorem 1.2 (Work-Energy Theorem). The work done by the net force on a particle equals the change in its kinetic energy:

W=r1r2Fdr=12mv2212mv12W = \int_{\mathbf{r}_1}^{\mathbf{r}_2} \mathbf{F} \cdot d\mathbf{r} = \frac{1}{2}mv_2^2 - \frac{1}{2}mv_1^2

Proof. Using Newton’s second law:

W=mavdt=mdvdtvdt=mvdv=12mv2212mv12W = \int m\mathbf{a} \cdot \mathbf{v}\, dt = \int m \frac{d\mathbf{v}}{dt} \cdot \mathbf{v}\, dt = \int m\mathbf{v} \cdot d\mathbf{v} = \frac{1}{2}mv_2^2 - \frac{1}{2}mv_1^2

\blacksquare

Definition. A force is conservative if the work done is path-independent, equivalently ×F=0\nabla \times \mathbf{F} = \mathbf{0}Equivalently F=V\mathbf{F} = -\nabla V for some scalar potential V(r)V(\mathbf{r}).

Theorem 1.3 (Conservation of Mechanical Energy). If all forces are conservative, E=T+VE = T + V is conserved.

Proof. For a conservative force, W=ΔVW = -\Delta V. By the work-energy theorem:

ΔV=ΔT    Δ(T+V)=0-\Delta V = \Delta T \implies \Delta(T + V) = 0

\blacksquare

Theorem 1.4 (Conservation of Angular Momentum). If the net external torque on a system vanishes, the total angular momentum is conserved.

Proof. The angular momentum of the ii-th particle about the origin is Li=ri×mivi\mathbf{L}_i = \mathbf{r}_i \times m_i \mathbf{v}_i. Taking the time derivative:

L˙i=r˙i×mivi+ri×miv˙i=ri×Fi\dot{\mathbf{L}}_i = \dot{\mathbf{r}}_i \times m_i \mathbf{v}_i + \mathbf{r}_i \times m_i \dot{\mathbf{v}}_i = \mathbf{r}_i \times \mathbf{F}_i

Since r˙i×mivi=vi×mivi=0\dot{\mathbf{r}}_i \times m_i \mathbf{v}_i = \mathbf{v}_i \times m_i \mathbf{v}_i = \mathbf{0}. Summing over all particles:

L˙=iri×Fi(ext)+ijiri×Fij\dot{\mathbf{L}} = \sum_i \mathbf{r}_i \times \mathbf{F}_i^{(\mathrm{ext})} + \sum_i \sum_{j \neq i} \mathbf{r}_i \times \mathbf{F}_{ij}

The double sum represents internal torques. For central internal forces (Fij\mathbf{F}_{ij} parallel to rirj\mathbf{r}_i - \mathbf{r}_j), the internal torques cancel in pairs. Hence:

L˙=τ(ext)\dot{\mathbf{L}} = \boldsymbol{\tau}^{(\mathrm{ext})}

If τ(ext)=0\boldsymbol{\tau}^{(\mathrm{ext})} = \mathbf{0} Then L=const\mathbf{L} = \mathrm{const}. \blacksquare

Definition. The rocket equation (Tsiolkovsky equation) describes the motion of a rocket that expels mass at a constant exhaust velocity.

Consider a rocket of mass mm moving with velocity vv in one dimension. In time dtdtIt ejects mass dmdm (where dm<0dm \lt 0) at exhaust velocity ueu_e relative to the rocket. The ejected mass has velocity vuev - u_e in the lab frame. By conservation of momentum:

mv=(m+dm)(v+dv)+(dm)(vue)mv = (m + dm)(v + dv) + (-dm)(v - u_e)

Neglecting the second-order term dmdvdm\, dv:

mv=mv+mdv+dmvdmv+uedmmv = mv + m\, dv + dm\, v - dm\, v + u_e\, dm

0=mdv+uedm0 = m\, dv + u_e\, dm

dv=uedmmdv = -u_e \frac{dm}{m}

Integrating from initial mass m0m_0 and velocity v0v_0 to final mass mfm_f and velocity vfv_f:

vfv0=uelnm0mfv_f - v_0 = u_e \ln\frac{m_0}{m_f}

This is the Tsiolkovsky rocket equation.

Theorem 1.5 (Rocket Equation with Gravity). If the rocket moves vertically against a uniform gravitational field gg:

Δv=uelnm0mfgΔt\Delta v = u_e \ln\frac{m_0}{m_f} - g\, \Delta t

Where Δt\Delta t is the burn time.

Problem. A rocket starts from rest with mass m0=1000kgm_0 = 1000\,\mathrm{kg} and exhaust velocity ue=3000m/su_e = 3000\,\mathrm{m}/s. It burns fuel until its mass is mf=400kgm_f = 400\,\mathrm{kg}. Find the final velocity.

Solution

Applying the Tsiolkovsky rocket equation:

Δv=uelnm0mf=3000ln1000400=3000ln(2.5)3000×0.916=2749m/s\Delta v = u_e \ln\frac{m_0}{m_f} = 3000 \ln\frac{1000}{400} = 3000 \ln(2.5) \approx 3000 \times 0.916 = 2749\,\mathrm{m}/s

\blacksquare

1.10 Worked Example: Elastic Collision in Two Dimensions

Section titled “1.10 Worked Example: Elastic Collision in Two Dimensions”

Problem. A particle of mass m1=2kgm_1 = 2\,\mathrm{kg} moving at v1=4i^m/s\mathbf{v}_1 = 4\hat{\mathbf{i}}\,\mathrm{m/s} collides elastically with a particle of mass m2=3kgm_2 = 3\,\mathrm{kg} at rest. After the collision, m1m_1 moves at 3030^\circ to the xx-axis. Find the final velocities.

Solution

Conservation of momentum (x-component): m1v1x=m1v1fcosθ1+m2v2fcosθ2m_1 v_{1x} = m_1 v_{1f}\cos\theta_1 + m_2 v_{2f}\cos\theta_2 2×4=2×v1fcos30+3×v2fcosθ22 \times 4 = 2 \times v_{1f}\cos 30^\circ + 3 \times v_{2f}\cos\theta_2

Conservation of momentum (y-component): 0=m1v1fsinθ1m2v2fsinθ20 = m_1 v_{1f}\sin\theta_1 - m_2 v_{2f}\sin\theta_2 0=2×v1fsin303×v2fsinθ20 = 2 \times v_{1f}\sin 30^\circ - 3 \times v_{2f}\sin\theta_2

Conservation of kinetic energy: 12m1v12=12m1v1f2+12m2v2f2\frac{1}{2}m_1 v_1^2 = \frac{1}{2}m_1 v_{1f}^2 + \frac{1}{2}m_2 v_{2f}^2 2×16=2×v1f2+3×v2f22 \times 16 = 2 \times v_{1f}^2 + 3 \times v_{2f}^2

From the y-component equation: v1fsin30=32v2fsinθ2v_{1f}\sin 30^\circ = \frac{3}{2}v_{2f}\sin\theta_2 0.5v1f=1.5v2fsinθ2    v2fsinθ2=v1f30.5 v_{1f} = 1.5 v_{2f}\sin\theta_2 \implies v_{2f}\sin\theta_2 = \frac{v_{1f}}{3}

From the x-component equation: 8=3v1f+3v2fcosθ28 = \sqrt{3} v_{1f} + 3 v_{2f}\cos\theta_2

From energy conservation: 32=2v1f2+3v2f232 = 2v_{1f}^2 + 3v_{2f}^2

Solving these equations simultaneously (using v2fsinθ2=v1f/3v_{2f}\sin\theta_2 = v_{1f}/3 and v2fcosθ2=(83v1f)/3v_{2f}\cos\theta_2 = (8 - \sqrt{3}v_{1f})/3):

v2f2=(v1f3)2+(83v1f3)2v_{2f}^2 = \left(\frac{v_{1f}}{3}\right)^2 + \left(\frac{8 - \sqrt{3}v_{1f}}{3}\right)^2

32=2v1f2+3[v1f29+(83v1f)29]32 = 2v_{1f}^2 + 3\left[\frac{v_{1f}^2}{9} + \frac{(8 - \sqrt{3}v_{1f})^2}{9}\right]

After algebraic manipulation: v1f1.6m/s,v2f2.9m/sv_{1f} \approx 1.6\,\mathrm{m/s}, \quad v_{2f} \approx 2.9\,\mathrm{m/s}

The second particle moves at approximately θ219\theta_2 \approx 19^\circ below the xx-axis.

\blacksquare

Common mistake. Assuming the second particle moves along the xx-axis. In two-dimensional elastic collisions, both particles generally move at angles to the original direction.

1.11 Worked Example: Non-Inertial Reference Frame

Section titled “1.11 Worked Example: Non-Inertial Reference Frame”

Problem. A block of mass m=5kgm = 5\,\mathrm{kg} sits on a frictionless horizontal surface inside an elevator accelerating upward at a=2m/s2a = 2\,\mathrm{m/s^2}. A horizontal force F=20NF = 20\,\mathrm{N} is applied. Find the acceleration relative to the elevator.

Solution

In the elevator frame (non-inertial), we must include the fictitious force ma-ma acting downward on the block. The forces in the horizontal direction are:

Applied force: F=20NF = 20\,\mathrm{N}

Fictitious force: ma=5×2=10N-ma = -5 \times 2 = -10\,\mathrm{N} (horizontal component, since the elevator accelerates vertically, the fictitious force is purely vertical)

Wait — the fictitious force is vertical, not horizontal. In the elevator frame, the block experiences:

  • Gravity: mgmg downward
  • Normal force: NN upward
  • Fictitious force: mama downward (since elevator accelerates upward)
  • Applied force: F=20NF = 20\,\mathrm{N} horizontal

The vertical forces cancel in the elevator frame (the block doesn’t accelerate vertically relative to the elevator). The horizontal acceleration relative to the elevator is:

arel=Fm=205=4m/s2a_{\text{rel}} = \frac{F}{m} = \frac{20}{5} = 4\,\mathrm{m/s^2}

In the ground frame, the horizontal acceleration is also 4m/s24\,\mathrm{m/s^2} (since the fictitious force has no horizontal component).

\blacksquare

Note. The fictitious force only affects motion in the direction of the non-inertial acceleration. If the elevator were accelerating horizontally, the fictitious force would be horizontal and would affect the block’s horizontal motion.

1.12 Worked Example: Centre of Mass of a System

Section titled “1.12 Worked Example: Centre of Mass of a System”

Problem. Three particles of masses m1=1kgm_1 = 1\,\mathrm{kg}, m2=2kgm_2 = 2\,\mathrm{kg}, m3=3kgm_3 = 3\,\mathrm{kg} are located at (0,0)(0,0), (2,0)(2,0), and (0,3)(0,3) respectively. Find the position of the centre of mass and the moment of inertia about an axis through the centre of mass perpendicular to the xyxy-plane.

Solution

Centre of mass coordinates: xcm=m1x1+m2x2+m3x3m1+m2+m3=1×0+2×2+3×06=46=23mx_{cm} = \frac{m_1 x_1 + m_2 x_2 + m_3 x_3}{m_1 + m_2 + m_3} = \frac{1 \times 0 + 2 \times 2 + 3 \times 0}{6} = \frac{4}{6} = \frac{2}{3}\,\mathrm{m}

ycm=m1y1+m2y2+m3y3m1+m2+m3=1×0+2×0+3×36=96=32my_{cm} = \frac{m_1 y_1 + m_2 y_2 + m_3 y_3}{m_1 + m_2 + m_3} = \frac{1 \times 0 + 2 \times 0 + 3 \times 3}{6} = \frac{9}{6} = \frac{3}{2}\,\mathrm{m}

Distances from each particle to the centre of mass: r1=(23)2+(32)2=49+94=97361.64mr_1 = \sqrt{\left(\frac{2}{3}\right)^2 + \left(\frac{3}{2}\right)^2} = \sqrt{\frac{4}{9} + \frac{9}{4}} = \sqrt{\frac{97}{36}} \approx 1.64\,\mathrm{m}

r2=(223)2+(032)2=(43)2+(32)2=169+94=145362.01mr_2 = \sqrt{\left(2 - \frac{2}{3}\right)^2 + \left(0 - \frac{3}{2}\right)^2} = \sqrt{\left(\frac{4}{3}\right)^2 + \left(\frac{3}{2}\right)^2} = \sqrt{\frac{16}{9} + \frac{9}{4}} = \sqrt{\frac{145}{36}} \approx 2.01\,\mathrm{m}

r3=(023)2+(332)2=(23)2+(32)2=97361.64mr_3 = \sqrt{\left(0 - \frac{2}{3}\right)^2 + \left(3 - \frac{3}{2}\right)^2} = \sqrt{\left(\frac{2}{3}\right)^2 + \left(\frac{3}{2}\right)^2} = \sqrt{\frac{97}{36}} \approx 1.64\,\mathrm{m}

Moment of inertia about the centre of mass: Icm=miri2=1×9736+2×14536+3×9736=97+290+29136=6783618.83kgm2I_{cm} = \sum m_i r_i^2 = 1 \times \frac{97}{36} + 2 \times \frac{145}{36} + 3 \times \frac{97}{36} = \frac{97 + 290 + 291}{36} = \frac{678}{36} \approx 18.83\,\mathrm{kg\cdot m^2}

\blacksquare

Common mistake. Using the origin instead of the centre of mass when calculating the moment of inertia. The parallel axis theorem relates the two: I=Icm+Md2I = I_{cm} + Md^2 where dd is the distance from the centre of mass to the rotation axis.

1.10 From Newton to Variational Principles

Section titled “1.10 From Newton to Variational Principles”

Newton’s laws work well in Cartesian coordinates but become cumbersome in constrained systems or Non-Cartesian coordinates. The Lagrangian and Hamiltonian formulations provide a more general And elegant framework based on energy principles.

The key insight: instead of tracking forces, track the energy of the system. The trajectory is the One that minimises (or more precisely, makes stationary) the action.

Mistake 1: Confusing mass with weight Mass is an intrinsic property of an object (measured in kg), while weight is the gravitational force on it (W=mgW = mg, measured in N). Students often use “weight” when they mean “mass” and apply F=mgF = mg without recognising that gg varies with location. On the Moon, your mass is the same but your weight is about one-sixth of Earth’s.

Mistake 2: Getting the direction of friction wrong Kinetic friction opposes the direction of motion relative to the surface, not the direction of the applied force. Static friction opposes the tendency of motion and can point in any direction along the surface. A common error is assuming friction always acts opposite to the applied force, which fails when the applied force has a component parallel to the surface that does not cause motion.

Mistake 3: Forgetting that Newton’s third law pairs act on different objects The action-reaction pair in Newton’s third law always acts on different objects. If object A exerts a force on object B, then object B exerts an equal and opposite force on object A. These forces do not cancel because they act on different bodies. A frequent mistake is adding action-reaction forces together and concluding the net force is zero.

flowchart TD
A[1_Newtonian Mechanics Review] --> B[Key Concepts]
A --> C[Core Principles]
A --> D[Practical Applications]
B --> E[Fundamental definitions]
C --> F[Design patterns]
D --> G[Real-world usage]